Abstract

In complex urban environments, a single Global Navigation Satellite System (GNSS) is often not ideal for navigation due to a lack of sufficient visible satellites. Additionally, the heading angle error of a GNSS/micro-electro-mechanical system–grade inertial measurement unit (MIMU) tightly coupled integration based on the single antenna is large, and the attitude angle, velocity, and position calculated therein all have large errors. Considering the above problems, this paper designs a tightly coupled integration of GNSS/MIMU based on two GNSS antennas and proposes a singular value decomposition (SVD)-based robust adaptive cubature Kalman filter (SVD-RACKF) according to the model characteristics of the integration. In this integration, the high-accuracy heading angle of the carrier is obtained through two antennas, and the existing attitude angle information is used as the observation to constrain the filtering estimation. The proposed SVD-RACKF uses SVD to stabilize the numerical accuracy of the recursive filtering. Furthermore, the three-stage equivalent weight function and the adaptive adjustment factor are constructed to suppress the influence of the gross error and the abnormal state on the parameter estimation, respectively. A set of real measured data was employed for testing and analysis. The results show that dual antennas and dual systems can improve the positioning performance of the integrated system to a certain extent, and the proposed SVD-RACKF can accurately detect the gross errors of the observations and effectively suppress them. Compared with the cubature Kalman filter, the proposed filtering algorithm is more robust, with higher accuracy and reliability of parameter estimation.

Highlights

  • The integration of the Global Navigation Satellite System (GNSS) and the StrapdownInertial Navigation System (SINS) is currently one of the main combined modes of application and research in the field of navigation and positioning [1]

  • Taking into account the characteristics of the GNSS/mechanical system–grade inertial measurement unit (MIMU) tightly coupled integration model and the high numerical accuracy and stability of CKF, this paper proposes a novel robust adaptive cubature Kalman filter based on singular value decomposition called

  • Dual GNSS antennas can assist in correcting attitude information such as carrier heading angles, which can be used as an option to enhance the navigation performance of low-cost MIMUs

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Summary

Introduction

The integration of the Global Navigation Satellite System (GNSS) and the Strapdown. Inertial Navigation System (SINS) is currently one of the main combined modes of application and research in the field of navigation and positioning [1]. The data fusion in tightly coupled navigation, especially fusing GNSS raw observations and micro-electromechanical system (MEMS)–grade inertial measurement unit (MIMU) data has become a hot topic in current research [2,3,4]. GNSS technology has completely changed the way of acquiring spatiotemporal information and promoted the efficiency with which people achieve it. It has the advantages of being applicable in all weather with high accuracy, high efficiency, high reliability, low cost, etc.

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